This chapter first reviews several aspects of the riveting process to ensure that riveted joints will have excellent fatigue performance. These aspects include solid rivets, joint design rules, several experimental and numerical methods to determine the residual stress/strain and interference in riveted joints, and the current approach for studying the riveting process. It then provides two case studies using experimental and finite element methods to explore: (i) the effect of the riveting process on the residual stress/strain in joints: and (ii) the stress condition in riveted lap joints when the joints are remotely loaded in tension. Concluding remarks on the potential development direction of the riveting tools and rivets are briefly pr...
International audienceAs one of the most reliable fasteners, solid riveted joints are widely utilize...
Aircraft fuselage skin panels are joined together by rivets. The initiation and propagation of fati...
Both experiments and finite element analysis were carried out to study the residual strain (stress) ...
Solid riveting is the most widely used joining technique in aircraft assembly, and the current key p...
Solid riveting is the most widely used joining technique in aircraft assembly, and the current key p...
The riveting process in the aerospace industry underlies high requirements to achieve the expected m...
The paper presents experimental and numerical study of the local phenomena during the riveting proce...
Riveted lap joints are being used traditionally for long in the aerospace industry. These joints are...
Riveted joints are a common location of fatigue cracks in aircraft metal structures. Fatigue life of...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
The riveting parameters strongly affect residual stresses induced during riveting, which in turn hav...
International audienceAs one of the most reliable fasteners, solid riveted joints are widely utilize...
Aircraft fuselage skin panels are joined together by rivets. The initiation and propagation of fati...
Both experiments and finite element analysis were carried out to study the residual strain (stress) ...
Solid riveting is the most widely used joining technique in aircraft assembly, and the current key p...
Solid riveting is the most widely used joining technique in aircraft assembly, and the current key p...
The riveting process in the aerospace industry underlies high requirements to achieve the expected m...
The paper presents experimental and numerical study of the local phenomena during the riveting proce...
Riveted lap joints are being used traditionally for long in the aerospace industry. These joints are...
Riveted joints are a common location of fatigue cracks in aircraft metal structures. Fatigue life of...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
In aeronautical and automotive industries the use of rivets for applications requiring several joini...
The riveting parameters strongly affect residual stresses induced during riveting, which in turn hav...
International audienceAs one of the most reliable fasteners, solid riveted joints are widely utilize...
Aircraft fuselage skin panels are joined together by rivets. The initiation and propagation of fati...
Both experiments and finite element analysis were carried out to study the residual strain (stress) ...